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Aerostructural wing shape optimization assisted by algorithmic differentiation

Structural and multidisciplinary optimization, 2021-08, Vol.64 (2), p.739-760

2021

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Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems

AIAA journal, 2019-05, Vol.57 (5), p.2158-2170

2019

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A Hybrid Reduced-Order Model for the Aeroelastic Analysis of Flexible Subsonic Wings—A Parametric Assessment

Aerospace, 2018-09, Vol.5 (3), p.76

2018

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Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future

Progress in aerospace sciences, 2016-11, Vol.87, p.1-93

2016

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Three-Dimensional Unsteady Aerodynamic Analysis of a Rigid-Framed Delta Kite Applied to Airborne Wind Energy

Energies (Basel), 2021-12, Vol.14 (23), p.8080

2021

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Minimum Induced Drag Theorems for Multiwing Systems

AIAA journal, 2017-10, Vol.55 (10), p.3266-3287

2017

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Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation

Composite structures, 2017-10, Vol.177, p.54-79

2017

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Feasibility studies on regional aircraft retrofitted with hybrid-electric powertrains

Aerospace science and technology, 2024-08, Vol.151, p.109246, Article 109246

2024

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Minimum Induced Drag Conditions for Truss-Braced Wings

AIAA journal, 2018-12, Vol.56 (12), p.4669-4684

2018

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Exploratory Structural Investigation of a Hawkmoth-Inspired MAV's Thorax

International journal of micro air vehicles, 2012-12, Vol.4 (4), p.291-304

2012

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Invariant Formulation for the Minimum Induced Drag Conditions of Nonplanar Wing Systems

AIAA journal, 2014-10, Vol.52 (10), p.2223-2240

2014

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Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy

AIAA journal, 2014-05, Vol.52 (5), p.964-980

2014

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Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Composite structures, 2015-11, Vol.131, p.501-515

2015

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Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis

European journal of control, 2020-07, Vol.54, p.49-63

2020

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Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications

Journal of optimization theory and applications, 2016-04, Vol.169 (1), p.236-261

2016

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Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory

Journal of optimization theory and applications, 2016-04, Vol.169 (1), p.200-235

2016

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Correction to: Optimum Induced Drag of Wingtip Devices: The Concept of Best Winglet Design

Aerotecnica, missili e spazio, 2022-06, Vol.101 (2), p.197-197

2022

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Reduced basis methods for structurally nonlinear Joined Wings

Aerospace science and technology, 2017-09, Vol.68, p.486-495

2017

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Optimum Induced Drag of Wingtip Devices: The Concept of Best Winglet Design

Aerotecnica, missili e spazio, 2022-03, Vol.101 (1), p.61-93

2022

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NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings

Aerotecnica, missili e spazio, 2019-03, Vol.98 (1), p.85-104

2019

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Aerodynamic and Structural Studies of a Flapping Wing in Forward Flight

AIAA journal, 2016-09, Vol.54 (9), p.2768-2781

2016

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Postcritical Analysis of PrandtlPlane Joined-Wing Configurations

AIAA journal, 2013-01, Vol.51 (1), p.161-177

2013

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Towards an Open-Source Framework for Aero-Structural Design and Optimization Within the SU2 Suite

Advances in Evolutionary and Deterministic Methods for Design, Optimization and Control in Engineering and Sciences, 2021, Vol.55, p.291-306

2021

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Risks of linear design of joined wings: a non-linear dynamic perspective in the presence of follower forces

CEAS aeronautical journal, 2015-06, Vol.6 (2), p.161-180

2015

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Phenomenology of nonlinear aeroelastic responses of highly deformable joined wings

Advances in aircraft and spacecraft science, 2015-04, Vol.2 (2), p.125-168

2015

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Aerostructural wing shape optimization assisted by algorithmic differentiation

Nonlinear Structural, Nonlinear Aerodynamic Model for Static Aeroelastic Problems

A Hybrid Reduced-Order Model for the Aeroelastic Analysis of Flexible Subsonic Wings—A Parametric Assessment

Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future

Three-Dimensional Unsteady Aerodynamic Analysis of a Rigid-Framed Delta Kite Applied to Airborne Wind Energy

Minimum Induced Drag Theorems for Multiwing Systems

Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation

Feasibility studies on regional aircraft retrofitted with hybrid-electric powertrains

Minimum Induced Drag Conditions for Truss-Braced Wings

Exploratory Structural Investigation of a Hawkmoth-Inspired MAV's Thorax

Invariant Formulation for the Minimum Induced Drag Conditions of Nonplanar Wing Systems

Nonlinear Analysis of PrandtlPlane Joined Wings: Effects of Anisotropy

Generalized Unified Formulation shell element for functionally graded Variable-Stiffness Composite Laminates and aeroelastic applications

Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis

Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications

Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory

Correction to: Optimum Induced Drag of Wingtip Devices: The Concept of Best Winglet Design

Reduced basis methods for structurally nonlinear Joined Wings

Optimum Induced Drag of Wingtip Devices: The Concept of Best Winglet Design

NERONE: An Open-Source Based Tool for Aerodynamic Transonic Optimization of Nonplanar Wings

Aerodynamic and Structural Studies of a Flapping Wing in Forward Flight

Postcritical Analysis of PrandtlPlane Joined-Wing Configurations

Towards an Open-Source Framework for Aero-Structural Design and Optimization Within the SU2 Suite

Risks of linear design of joined wings: a non-linear dynamic perspective in the presence of follower forces

Phenomenology of nonlinear aeroelastic responses of highly deformable joined wings

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